Influence of lobe geometry on mixing and heat release characteristics of solid fuel rocket scramjet combustor

标题
Influence of lobe geometry on mixing and heat release characteristics of solid fuel rocket scramjet combustor
作者
关键词
-
出版物
ACTA ASTRONAUTICA
Volume 164, Issue -, Pages 212-229
出版商
Elsevier BV
发表日期
2019-08-21
DOI
10.1016/j.actaastro.2019.08.005

向作者/读者发起求助以获取更多资源

Discover Peeref hubs

Discuss science. Find collaborators. Network.

Join a conversation

Become a Peeref-certified reviewer

The Peeref Institute provides free reviewer training that teaches the core competencies of the academic peer review process.

Get Started